As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING -C- CHECK, LWR VERTICLE LEADING EDGE LWR INTERNAL WEB CRACKS OUT AROUND BOLT FIN STA 55.9. REMOVED DAMAGED WEB AND FABBED NEW FROM 2024-T3 .032 PO 900534 DIM 12.75 X 12 INCH IAW 727 SRM 55-30-2 FIG 2. WEB TREATED & PRIMED IAW 727 SRM 51-10-2 & INSTALLED IAW 727 SRM 51-30-2.